International Journal of Aeronautical and Space Sciences

  • 제12권3호
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  • Pages.260-265
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  • 2011
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  • 2093-274X(pISSN)
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  • 2093-2480(eISSN)
한국항공우주학회 (The Korean Society for Aeronautical and Space Sciences)
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Time-Delay Control for Integrated Missile Guidance and Control

  • Park, Bong-Gyun (Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology) ;
  • Kim, Tae-Hun (Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology) ;
  • Tahk, Min-Jea (Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology)
  • 투고 : 2011.04.30
  • 심사 : 2011.09.06
  • 발행 : 2011.09.30
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초록

In this paper, integrated missile guidance and control systems using time-delay control (TDC) are developed. The next generation missile requires that an interceptor hits the target, maneuvering with small miss-distances, and has lower weight to reduce costs. This is possible if the synergism existing between the guidance and control subsystems is exploited by the integrated controller. The TDC law is a robust control technique for nonlinear systems, and it has a very simple structure. The feature of TDC is to directly estimate the unknown dynamics and the unexpected disturbance using one-step time-delay. To investigate the performance of the integrated controller, numerical simulations are performed as the maneuver of the target. The results show that the integrated guidance and control system has a good performance.

키워드

참고문헌

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피인용 문헌

  1. Single Versus Two-Loop Full-State Multi-Input Missile Guidance vol.38, pp.5, 2015, https://doi.org/10.2514/1.G000171
  2. Single Versus Two-Loop Full-State Guidance and Control vol.40, pp.8, 2017, https://doi.org/10.2514/1.G002722
  3. Linear Quadratic Integrated Versus Separated Autopilot-Guidance Design vol.36, pp.6, 2013, https://doi.org/10.2514/1.61363
  4. Continuous-Time Predictive Control-Based Integrated Guidance and Control vol.40, pp.7, 2017, https://doi.org/10.2514/1.G002661
  5. Full-State Autopilot-Guidance Design Under a Linear Quadratic Differential Game Formulation vol.47, pp.3, 2014, https://doi.org/10.3182/20140824-6-ZA-1003.01240
  6. Adaptive Integrated Guidance and Control Design for a Missile With Input Constraints vol.46, pp.20, 2013, https://doi.org/10.3182/20130902-3-CN-3020.00114
  7. Integrated versus two-loop guidance-autopilot for a dual control missile with high-order aerodynamic model vol.230, pp.1, 2016, https://doi.org/10.1177/0954410015586862
  8. Improved line of sight robot tracking toward a moving target vol.6, pp.3, 2018, https://doi.org/10.1080/21642583.2018.1547886